ASAP Part Services, owned and operated by ASAP Semiconductor, has over 6 billion parts inventoried. This includes new, old, used, and obsolete parts, such as 6897080, 6867378, 6867377, 9528M68P04, 4060966. As an ISO 9001:2015 certified and FAA AC 00-56B accredited company, we go to great lengths to ensure we are delivering quality parts. We partner exclusively with reliable manufacturers such as Allison Transmission Inc, Beacon Industries Inc, Cfm International Inc, Dover Tool Of Connecticut Llc, Ge Engine Services Llc. Our team provides superior quality assurance testing for III End Item Identification: Acft eng tf 41 Criticality Code Justification: AGAV Material: Steel corrosion resisting, III End Item Identification: TF-41 aircraft engine Criticality Code Justification: AGAV Material: Steel corrosion resisting, III End Item Identification: TF-41 aircraft engine Criticality Code Justification: AGAV Material: Steel corrosion resisting, III End Item Identification: Acft eng F100-PW-220 Criticality Code Justification: AGAV Special Features: Matl ams 5707 and more. So if you are in need of Retainer,Turbine Blade,Aircraft or any other NSN parts, submit an Instant RFQ and receive a quote in as little as 15 minutes.
| Manufacturers for Retainer Turbine Blade Aircraft | |||
|---|---|---|---|
| allison transmission inc | beacon industries inc | ||
| cfm international inc | dover tool of connecticut llc | ||
| ge engine services llc | general electric company | ||
| Part Number | NSN | Details | QTY | RFQ |
|---|---|---|---|---|
| 6897080 | 2840-01-124-4770 | iii end item identification: acft eng tf 41 criticality code justification: agav material: steel corrosion resisting | Avl | RFQ |
| 6867378 | 2840-00-415-0363 | iii end item identification: tf-41 aircraft engine criticality code justification: agav material: steel corrosion resisting | Avl | RFQ |
| 6867377 | 2840-00-415-0372 | iii end item identification: tf-41 aircraft engine criticality code justification: agav material: steel corrosion resisting | Avl | RFQ |
| 9528M68P04 | 2840-01-146-9374 | NA | Avl | RFQ |
| 4060966 | 2840-01-215-3548 | iii end item identification: acft eng f100-pw-220 criticality code justification: agav special features: matl ams 5707 | Avl | RFQ |
| 335-023-401-0 | 2840-01-669-8374 | NA | Avl | RFQ |
| 1475M84P01 | 2840-01-146-9374 | NA | Avl | RFQ |
| 1531M86P05 | 2840-01-617-5083 | NA | Avl | RFQ |
| 9697M33P12 | 2840-01-067-2684 | iii end item identification: acft eng tf39-ge1c criticality code justification: agav stage number: 1 | Avl | RFQ |
| 9697M33P10 | 2840-01-067-2684 | iii end item identification: acft eng tf39-ge1c criticality code justification: agav stage number: 1 | Avl | RFQ |
| 9697M33P09 | 2840-01-067-2684 | iii end item identification: acft eng tf39-ge1c criticality code justification: agav stage number: 1 | Avl | RFQ |
| 9697M33P07 | 2840-01-067-2684 | iii end item identification: acft eng tf39-ge1c criticality code justification: agav stage number: 1 | Avl | RFQ |
| 9697M33P01 | 2840-00-112-9644 | iii end item identification: acft eng tf-39 criticality code justification: agav special features: turbine stage 1 | Avl | RFQ |
| 9697M33P01 | 2840-01-067-2684 | NA | Avl | RFQ |
| 9697M24P01 | 2840-00-112-9645 | iii end item identification: acft eng tf39 criticality code justification: agav special features: for stage 2 | Avl | RFQ |
| 9687M66P01 | 2840-00-112-9644 | iii end item identification: acft eng tf-39 criticality code justification: agav special features: turbine stage 1 | Avl | RFQ |
| 9687M66P01 | 2840-01-067-2684 | NA | Avl | RFQ |
| 9666M52P01 | 2840-00-112-9645 | iii end item identification: acft eng tf39 criticality code justification: agav special features: for stage 2 | Avl | RFQ |
| 9528M68P04 | 2840-01-146-9374 | NA | Avl | RFQ |
| 9528M68P02 | 2840-01-146-9374 | NA | Avl | RFQ |
| 9527M71P02 | 2840-01-146-7483 | iii end item identification: acft eng f101 criticality code justification: agav material: steel | Avl | RFQ |
| 9514M75P05 | 2840-01-232-1961 | NA | Avl | RFQ |
| 9104M10P07 | 2840-01-138-5658 | iii end item identification: acft eng tf39 criticality code justification: agav special features: high pressure turbine rotor assy;2nd stage; cbore for 29 holes eq sp, 29 pockets | Avl | RFQ |
| 9104M10P06 | 2840-01-138-5658 | iii end item identification: acft eng tf39 criticality code justification: agav special features: high pressure turbine rotor assy;2nd stage; cbore for 29 holes eq sp, 29 pockets | Avl | RFQ |
| 9104M10P02 | 2840-00-112-9645 | iii end item identification: acft eng tf39 criticality code justification: agav special features: for stage 2 | Avl | RFQ |
| 9104M10P01 | 2840-00-112-9645 | iii end item identification: acft eng tf39 criticality code justification: agav special features: for stage 2 | Avl | RFQ |
| 5127T19P03 | 2840-01-526-3994 | NA | Avl | RFQ |
| 5127T19 | 2840-01-526-3994 | NA | Avl | RFQ |
| 5104T50P08 | 2840-01-536-3267 | iii end item identification: ge f414-400 engine iii part name assigned by controlling agency: retainer, turbine | Avl | RFQ |
| 5104T50P06 | 2840-01-443-2803 | iii end item identification: ge f414-400 engine | Avl | RFQ |
| 5078T28G03 | 2840-01-519-5977 | iii end item identification: ct7 turboprop engine iii part name assigned by controlling agency: shroud and w-seal, retainer, stage 2 | Avl | RFQ |
| 5060T89P05 | 2840-01-506-0260 | iii end item identification: ct7-9 turboprop engine | Avl | RFQ |
| 4082T52P01 | 2840-01-506-0249 | iii end item identification: ct7-9 turboprop engine | Avl | RFQ |
| 3074T70P02 | 2840-01-700-5775 | NA | Avl | RFQ |
| 2087M81P01 | 2840-01-522-6408 | iii end item identification: f110 slep hpt rotor | Avl | RFQ |
| 2087M79P02 | 2840-01-522-6407 | iii end item identification: f110 slep hpt rotor | Avl | RFQ |
| 2087M79P01 | 2840-01-522-6407 | iii end item identification: f110 slep hpt rotor | Avl | RFQ |
| 1668M81P02 | 2840-01-434-1990 | iii end item identification: f110-ge-100 aircraft gas turbine engine criticality code justification: abhp and abkv and feat special features: retainer for the low pressure turbine rotor, stage 1 | Avl | RFQ |
| 1668M50P02 | 2840-01-365-2220 | iii end item identification: acft eng f110-ge129 criticality code justification: agav material: steel | Avl | RFQ |
| 1522M94P05 | 2840-01-232-1961 | iii end item identification: acft.eng. f110 material: steel overall length: 0.492 inches minimum and 0.498 inches maximum | Avl | RFQ |
| 1498M20P02 | 2840-01-522-6409 | iii end item identification: f110 slep hpt rotor | Avl | RFQ |
| 1475M84P01 | 2840-01-146-9374 | NA | Avl | RFQ |
| 1387M99P04 | 2840-01-434-7060 | iii end item identification: f110-ge-100 aircraft gas turbine engine criticality code justification: abhp and abkv and feat special features: used on the low pressure turbine;matl nickel, cobalt, chromium alloy | Avl | RFQ |
| 1387M99P03 | 2840-01-434-7060 | iii end item identification: f110-ge-100 aircraft gas turbine engine criticality code justification: abhp and abkv and feat special features: used on the low pressure turbine;matl nickel, cobalt, chromium alloy | Avl | RFQ |
| 1387M99P01 | 2840-01-434-7060 | iii end item identification: f110-ge-100 aircraft gas turbine engine criticality code justification: abhp and abkv and feat special features: used on the low pressure turbine;matl nickel, cobalt, chromium alloy | Avl | RFQ |
| 1387M99 | 2840-01-434-7060 | iii end item identification: f110-ge-100 aircraft gas turbine engine criticality code justification: abhp and abkv and feat special features: used on the low pressure turbine;matl nickel, cobalt, chromium alloy | Avl | RFQ |
| 1385M57P06 | 2840-01-485-6705 | iii end item identification: f118-ge-100; xf118-ge-100 criticality code justification: agav special features: per cid 838238, ecp fh221, p06 replaces p01 and p05 | Avl | RFQ |
| 1385M57P05 | 2840-01-485-6705 | iii end item identification: f118-ge-100; xf118-ge-100 criticality code justification: agav special features: per cid 838238, ecp fh221, p06 replaces p01 and p05 | Avl | RFQ |
| 1385M57P01 | 2840-01-485-6705 | iii end item identification: f118-ge-100; xf118-ge-100 criticality code justification: agav special features: per cid 838238, ecp fh221, p06 replaces p01 and p05 | Avl | RFQ |
| 1275M13P04 | 2840-01-448-9591 | NA | Avl | RFQ |
| Relevant nsn Components For Retainer Turbine Blade Aircraft | |||
|---|---|---|---|
| 1 dl turret trainer | 3 dl turret trainer | 73a buffer retract | 73b buffer retract |
| a piston retainer | a system return air | accessori di retico | accessories retrofi |
| adapter assembly carburetor | adapter ball retaining | adapter carburetor | adapter carburetor to air cleane |
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